||This article includes a list of references, but its sources remain unclear because it has insufficient inline citations. (November 2012)|
|YB-60 prototype, Convair B-36F in the background|
|First flight||18 April 1952|
|Status||Canceled 14 August 1952|
|Program cost||US$14.3 million for program|
|Developed from||Convair B-36|
Design and development
On 25 August 1950, Convair issued a formal proposal for a swept-winged version of the B-36 with all-jet propulsion. The United States Air Force was sufficiently interested that on 15 March 1951, it authorized Convair to convert two B-36Fs (49-2676 and 49-2684) as B-36Gs. Since the aircraft was so radically different from the existing B-36, the designation was soon changed to YB-60.
The YB-60 had 72% parts commonality with its piston-engined predecessor. The fuselages of the two aircraft were largely identical, although the YB-60 had a longer, pointed nose with a needle-like instrument probe instead of the B-36's rounded nose; its tail surfaces were swept to match the wings and a wedge-shaped insert added at the wing root. The swept wings also used many B-36 parts.
The YB-60's unofficial competitor for an Air Force contract was Boeing's B-52 Stratofortress. Convair's proposal was substantially cheaper than Boeing's, since it involved modifying an existing design rather than starting from scratch. Like the B-52, it was powered by eight Pratt & Whitney J57-P-3 turbojets mounted in pairs in four pods suspended below the wing.
Instead of the B-36's crew of 15, the YB-60's crew numbered 10. Production B-60s were to have defensive armament similar to those of the B-36.
Convair YB-60 serial number 49-2676 made its maiden flight on 18 April 1952, piloted by Beryl Erickson. The Boeing YB-52 beat the Convair aircraft into the air by three days. The YB-60 was approximately 100 mph (160 km/h) slower than the YB-52 and also had severe handling problems. It carried a heavier bomb load — 72,000 lb (33,000 kg) against 43,000 lb (20,000 kg) for the YB-52 — but the Air Force did not see the need for the extra capacity, given the YB-60's other drawbacks. Later, "big belly" modifications increased the B-52's bomb load to 60,000 pounds (27,000 kg).
The flight test programs were canceled on 20 January 1953, with 66 flying hours accumulated. A second prototype was never completed: The airframe was built, but it was not fitted with engines or much equipment. Since Convair completed their prototype contract satisfactorily, both YB-60s were formally accepted by the Air Force in 1954. The operational aircraft never flew again, and both airframes were scrapped by July.
- Crew: five (two pilots, navigator, bombardier/radio operator, radio operator/tail gunner)
- Length: 171 ft (52.1 m)
- Wingspan: 206 ft (62.8 m)
- Height: 60 ft 6 in (18.4 m)
- Wing area: 5,239 ft2 (486.7 m2)
- Empty weight: 153,016 lb (69,407 kg)
- Loaded weight: 160,000 lb (73,000 kg)
- Max. takeoff weight: 300,000 lb (140,000 kg)
- Powerplant: 8 × Pratt & Whitney J57-P-3 turbojets, 8,700 lbf (38 kN) each
- Maximum speed: 508 mph (411 knots, 818 km/h) at 29,250 ft (8,915 m)
- Stall speed: 115 knots (132 mph, 212 km/h)
- Combat radius: 2,920 mi (2,540 nm, 4,700 km)
- Ferry range: 8,000 mi (7,000 nm, 13,000 km)
- Service ceiling: 53,300 ft (16,200 m)
- Rate of climb: 1,060 ft/min (5.38 m/s)
- Wing loading: 31 lb/ft2 (150 kg/m2)
- Thrust/weight: 0.44
- Related development
- Aircraft of comparable role, configuration and era
- Related lists
- Jacobsen, Meyers K. and Wagner, Ray. B-36 in Action (Aircraft in Action No.42). Carrollton, TX: Squadron/Signal Publications, Inc., 1980. ISBN 0-89747-101-6.
- Jones, L.S. U.S. Bombers, B-1 1928 to B-1 1980s. Fallbrook, CA: Aero Publishers, Inc., 1962 (second edition 1974). ISBN 0-8168-9126-5.
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